The Neutral Axis in Beam

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    THE

    NEUTTRAL

    AXIS

    IN

    BEAAIS-BJY Professor Hemy

    Adams M.llzst. C.E. F.R.I.B.A.

    Etc.

    When a rectangularbeam ssupportedat

    bothendsand oaded ransversely heupper

    fibres are compressed and the lower extended,

    the stresses being greatest in the outer fibres,

    and proportionally less towards th e middle of

    the depth, until a la,yer is reached where they

    bothvanish.Thismay be shownexperirnen-

    ta,lly by marking parallel vertical lines upon a

    beam of indiarubber as Fig . 1, and supporting

    it at heendswitha loadon top,when he

    lines will be found closer together In the upper

    part of thebeamand urtherapart n he

    lower, asFig . 2, while a t some ntermediate

    depth their distances will be unaltered, as in

    line Q

    b

    marking the neutxal layer, or neutral

    axis of the cross sect ion,and showing that

    reither tensionnorcompressionexists here.

    If

    A , S , C , D, Fig. 3 represent a cross section

    through the centreof a beam under transverse

    load, the maximum intensity of compres-

    sion drawn o sca,le, and

    g

    h themaximum

    intens ity of tension, then when t,hese stresses

    areroduced,he neutral1 axis will pass

    through the intersection

    k

    of lines e h

    f g ,

    and

    when f and gh are equal this will also be the

    cen tre of gravi ty of the eam.Whenhe

    stressndtrainre roportionaloach

    other, and equal n ension and compression,

    the horizontal lines will show by their length

    the ntensi ty of the tensileandcompressive

    stressrespectively n he various ayers.

    The position of the neut ral axis is a matter

    of great importance and is

    a

    subject that has

    exercised theminds of mathematiciansand

    engineers from the ti me of Galileo In 1638 up

    t o thepresentday.Leibnitz (1684) placed i t

    in the xtreme fibre of t he .concave side.

    Mariotte (1686) assumed hat half the fibres

    werextendednd half compressed. Ber-

    noulli (1705) came to the conclusion th at th e

    position was indifferent, tha t s o ay he

    whole of th e fibres might be in either tension

    or

    compression, the neut ral layer being on the

    surface furthest from the side where the stress,

    was rea tes t. Coulomb (1773) is considered

    by

    mathcmaticia.ns ohavebeen hefirst o

    lay down therue principles. According to

    Todhunter’s “ History of Elasticity,

    p. 120,

    Coulombplaced the neutra l (linealong the

    axis or middle ine of thebeam, becausehe

    argued hat t.he sum of the ongitudinal en-

    sions or resistances uf the fibresacrossany

    section must be zero if the beam be only acted

    on by a system of transverse forces.’’ “This,”

    says

    ‘Iodhunter,

    is

    a

    clearesult of an

    elementary principle of statics-the sum of

    the forcesresolvedparallel to the axis of the

    beam must be zero.”Riccati (1782) placed

    theneutralsurface n heextreme ayer

    on

    t,he concave side, supposing the whole beam to

    be under varyingdegrees of tension,ashad

    Leibnitz before him.

    Dr. Thomas Young

    (1802) was of opinion that the position of the

    neutral axis was dependent upon thenature

    of t,he material as regards its comparative re-

    sistance to tension and compression, and that,

    in general, it was nearer the .concave surface.

    Peter Harlow in

    An Essay on the Strength

    andStress of Timber ” (1817) assumed ha t

    the sum of the moments of the tensions

    of

    the extended fibres about the neutral point

    of

    any section, must be equa l to the sum of the

    moments of thecompressed fibres.

    Eaton

    Hodgkinsonobjected to his,butPeterBar-

    low

    in 1826 still houghthis view to be cor-

    rect ;however, in 1837 as the result of his own

    experiments, ewent over tohe side

    of

    Coulomb andHodgkinson. I n 1824 Hodgkin-

    son showed by experiment tha t the moduli

    of

    elasticity were not hesamefor ensionand

    ccmpressim

    of

    certain materials, notably cast

    iron, and that in a prismatic beam the neutral

    line would ingeneralnot coincide with the

    axis of figure. He st at ed he law as follows:

    I n the bending of any body this proportion

    ill obtain as the extension of the outer fibre

    on one side is to the contraction of that on the

    other, so is the distance of the former frorn the

    neutral line

    to

    tha t of the atter .” This

    ap-

    pears ome o be the rue heory,but on

    account of mathematicians assuming that for

    equal stresses lleextensionand compression

    are equal, they arc led to the conclusion that

    the eutra l axissnvariably fixed athe

    centre of gravity of the section,although n

    stat ing the proposition they generally lirnlt the

    circumstances to “ a small deflection.”

    This proposition may be found in Rankine’s

    Civitl Engineering,--p.251, Twisden’s Practical

    Mechanics,

    p.

    182,IJnwin’s MachineDesign,

    1882, p .

    39,

    Perry’sractical fiIecllanics,

    p. 105

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    THE

    STRUCTURAL

    NGINEER. 2 7 5

    Humber Handy Book of Strains, p. 61) ceptibly from the central line.

    2 )

    Amounts of

    says,

    provided that he im it s of elasticity extension and compression in t.he case of

    of the mat erial of the beam be

    not

    exceeded,

    wrought roncontinue o be equalup o he

    the neutr al axis will pass through the centre

    completeestruction

    of

    the elasticity. ( ?

    of gravity

    of

    elastic limit.

    the section.’’

    3)

    T h e yHe does not

    a r en l y

    say what will

    equal in the

    happen when

    case

    of

    cast

    the imits of

    x

    ironpo

    elasticity are

    exceeded.

    FIG. I

    Anderson (Strength of Materials, . 167

    adoptsarlow’sirst opinion, th athe

    mom ents of tension and compression on either

    side of theneutra l axis mus t be equal,and

    form a couple, kep t n equilibrium y the

    couple formed by the load and react ion. This

    isavery easible view but akes

    no

    account

    of th e re ht iv e extension and compression.

    “ An ounce of practice sworth a. pound

    of

    theory,’’ and an account of actualexperi-

    ments will doubtless be of greater general in-

    terest hananelaborate nvestigation of the

    rnathematicalprinciples.

    In

    1841 the esults

    of

    some experirnents upou rectangular beams

    of cast and wrought-iron and wood were pre-

    I about 2.3rds

    of-_

    breaking

    load, after this load extension yielded in a higher

    ratio than compression.

    (4)Wit h fir battens, extension and compres-

    sionwere equalup o of t,hebreaking oad,

    but after this compression yielded in a much

    higherratio hanextension.

    5 )

    Amounts

    of

    extensionand compression

    are in direct proportion to the st ra in ( ? stress)

    within the limi ts of. elasticity and even after

    those imitsaregreatlyexceeded,and up to

    of the stre ngth of a beam they

    do

    not sensi-

    bly differ.

    Box (Strength of Materials ,p.

    326)

    gives

    some nformation

    on th e extension and com-

    pression

    of

    cast and wrought iron under stress,

    sented the and s t a t e s

    Institution of thatt 2.355

    C i v i l tons per sq.

    gineers in a c in. the exten-

    memoir b

    y

    sion and

    com-

    Joseph Colt pression

    o

    f

    hurst (Min. cast ironre

    Proc. Inst. e q u a l , and

    C.E.,

    1841). h e n c ei t

    The object of

    W i 11 follow

    the experi t h a th e

    merits was toascertainpractical ly he posi- neut raj axis wiEl be in hecen tre of the sec-

    ,.ion of theeutra l axis andheelativeion.”With lower stresseshe compressions

    amount

    of compressionandextension at he

    exceed tne eiitensions andithigher

    stresses he extensionsexceed the compres-

    upper and under surfaces

    of

    the beams when

    sions.

    subjected o ransverse oad.Theresults ob-

    I n a paper

    on

    “ The Optical Expression of

    tainedare briefly summarised

    as

    follows:- Stress ,’’ by James Love Transactions

    Civ.

    1)

    Position of neutral line in materials of the

    and Mech. Eng. Society, February,

    1877)

    the

    formstated n he it le , does not differ per-

    mathematical heory is said to be absolutely

    FIG 2 .

    Irish

    Branch.

    South-

    FVestern

    Branch.

    TheHon. ecretary,owhomllom-

    The Hon. Secretary,o whom all com-

    munications houldbe ddressed, ndrom munications should be addressed, androm

    .whom particulars may be obtained, is Mr. P.

    whom particularsmay be .obtained, is Mr.

    Kearney,.I.Struct.E.,

    3,

    Lower Abbey

    F.

    H . Waple, A.LStruct.E.,

    28

    Ker Street,

    Street,Dublin.

    Devonport. ~ .

  • 8/16/2019 The Neutral Axis in Beam

    3/8

    proved by experiments on glassbeamsunder

    stressobserved hrough a polariscope, but in

    this case the stresseswere probably well within

    the elastic llinlit.

    Theracticalngineer's view,

    as

    dis-

    tinguishedfrom hemat'hematician's, s hat

    the neutra axispasses ,hrough the centre of

    gravity at the com-

    mencement of the

    bending, and that

    when rupture takes

    place it will have

    shifted to such .a

    point that the outer

    fibres will have

    reached theirlti-

    mate resistance to

    tension and com-

    pression r

    e

    s

    p

    e

    c-

    tively, the tot11

    depth being divided

    in he inverse ratio

    of theultimate e-

    I3

    D

    L

    FIG

    1

    sistancees to tension and compression

    ,

    (Armour),

    or the inverse ratio

    of

    theirquare, roots

    (Anderson).

    Now

    we come to

    H

    pointwhere the tliver-

    gence of the various modern opinions mu st be

    considered in more detail.

    We have first the opinion ,t8hat in a homo-

    geneous beam of any material of rectangular

    CIUSS

    sectiona)heeutral axisasses

    through hecentre of gravity of the section,

    (b) thestress varies directqy as he distance:

    from the neutral gxis, and (c) the extr eme fibre

    stresss equa. inension nd ompression.

    This s ndicated nFig. 3, where ef repre-

    sents the rna,ximum compression, gh tlhe maxi-

    11111111 tension, and, being equal to each ,other,

    the ntersection of the ines

    eh ,

    fg ,

    a t

    k will

    show the neu tra l axis at the cent re of gravity

    of the setetion. It is well known ,thatwith

    manymaterials hestrength. snotequal n

    tension and compression b ut upon this theory

    failure mustake placewhen the xtreme

    limit .of strength of the weaker side is reached.

    Next we have he opinion that hestress

    vnries tlirect'ly as the distal7ce

    f 1 w n l

    t,he

    neutra

    axis as before, but tha t the maximum stresses

    arereachedboth n ensionand conlpression

    b y reason of the neutra l axis shifting towards

    the weaker side,

    as

    shown in Fig. 4

    A4sh

    and

    .,Fig

    4ar

    Oast Iron: .In each case

    t

    t +C

    '

    . .

    .

    . .

    .

    x:

    ~.-

    X

    d

    , .

    where

    t

    =ultimateensile trength, =ulti-

    mate compressive strength.

    If we call theshaded riangles he nertia

    areas , then another opinion is tha t the tensile

    inertiaareamustequal he conlpressive in-

    ertia rea,makinghe eutra l axis e,arer

    the greater stress intensity, so that the total

    tensile stress shall equal the total cornpressive

    stmss, as in Fig 5 Ash and Fig Sa Cast I r o n .

    I n

    eachcase

    X =-

    x dThispermits he

    stresses to form a couple of which the arm is

    C

    c + t

    Stillanother opinion is hat hemoments

    of

    the iner tia ar eas must be equal

    so

    that they

    brlance bouthe eutral xis, which will

    make the neutral axis nearer the greater stress

    intensity, as in the last case, but

    as in Fig 6 Ash and Fig.

    6a

    Cast Iron.

    l t will be interesting now to compare t'hese

    variouspinions by calculationsromhe

    actua strengths of the two materials named,

    Ash

    andCastIron. Before doing

    so

    itmust

    be

    stated hat although it would seem elf-

    evident tha t the extr eme fibre stresses under

    U

    transverse breaking load would agree with the

    masinlum tensi le and compressive resistances

    underdirect ensile

    or

    compressive s tress, t

    is found by experiment that they do not coin-

    cide, bu t that the value varies with the form

    of the cross-section of thematerial.Several

    theories have' been propounded in explanation

    of thispeculiarity, houghnone

    of

    them s

    entirelyatisfactory. R,ankine assumes one

    cause to be the fac t that' the resistance of a

    material odirectstress s ncreased bypre-

    venting

    or

    diminishing thealtera tion of it s

    trmsverse dim,ensions. H e alsosuggests that

    when bar of31etgl isorn sunderhe

    strength. indicated is .that

    of

    the centre part,

    which is the weakest, whilst when it i s broken

    transversetly the strength indicated is that of

    the outer part, which is the strongest. In th e

    case of timber it is sugges ted that the lateral

    adhesion of the fibres prevents the outer ones

    flom moving freely and hence in all cases the

    actual extreme stress is considerably less than

    it, appears by calculation. Inanyevent,

    the

    difference eally exists ,and nstead of deter-

    mining the ikodulus of rupture from the ten-

    sile and compressive strength, it can only be

    h n d by actual expepiment on cross-breaking.

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    THESTRUCTURALNGINEER.

    277

    In he fornlls tt 'c

    = Z C ,

    C is ~lorninally

    the extreme fibre stress but, it is really o more

    than he coefficient of rupture for transverse

    strength derived rom experiment. Of course

    it bears some rehtion to the maximum dir ect

    stresses n ensionand compression but can-

    not. be derivedrom them.he section

    modulus Z provides orvariation due o he

    form of section.Sir B. Baker

    showed

    that

    for a rectangularectionhe pparent e s -

    trcme fibre stress was

    70

    per cent. nexcess

    o f

    the direct strength of the mate rial, and for

    anyother orm of section the ame propor-

    tion of 70 per cent. as the area of the section

    bears to the area of B circumscribing rectangle.

    l .

    Claston Fidler in his Bridge Construc-

    tion

    * 11lrzkes

    :I statement to the same effect.

    H e

    says:-

    The implicity of th is tlheory w o u ~ dbe

    very

    satisfactory if i t could

    be

    regarded

    as a

    true and complete statement of the facts; for

    not'hingcould beeasie r han o calcu ate by

    t,he ast. ormula t'hc weigFt required to pro-

    4

    Ash

    l

    I

    duce any given tensile stress ; and if we know

    the ultimate ensile strengt'h of the material,

    i t would seem t,hat we ought t'o

    be

    able, by

    this means, to find exactly the load that will

    break

    the

    beam. Bat if we take a rectangulw

    beam

    of

    cast-iron nd uthe ahlated

    breaking load upon it , th e

    beam

    will shcw no

    sympt80n1s

    of

    .tearingat hestretchedfibres,

    and no ndina tion o yield in any way; and

    as a matter of fact it will not break until we

    have increased the load t'o about 2 times the

    amountcalculated."

    I n girder and roof work it is the practtice

    of

    engineers to calculate heresistancemoment

    of

    any beam by assuming

    C:

    to be the maxi-

    mum working

    stress

    allowed on the material,

    taking s or the tension side and Zy for the

    compression ide, ,he neutra l axisbeing

    as-

    sumed

    t o

    pass

    through the centre of gravity

    of

    the

    section.

    Now

    takeasanexample

    for

    calculation

    a

    beam of ash

    6

    in. broad, 9 in. deep and

    20

    tt.

    slxm loaded to breaking by a dead load in the

    W

    \ C

    X

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    2 7 8 THE STKUCTURALNGINEER: he Journal

    centr e. The weight of beam may be omit ted.

    Thedata

    for

    ash, aking he average of all

    available records are

    Max. direct tension ... 14,500 lbs. sq. in.

    Transverse breaking load on

    centre of unit beam

    1

    n.

    C or modulus

    of

    transverse

    .. compression

    ...

    7,400 ..

    by 1 n. by

    1

    ft. span ... 834 lbs.

    strength .....

    ...

    15,000 lbs.

    By

    the ransversebreaking load

    of

    aunit

    heam, heultimate trength of thepresent

    beam will be

    W= 834X --= 834X E 1= 20266*2

    d'

    lb.

    L

    20

    in centre.

    By the method of Fig. 3 , x=y=+d.=4& in .

    nesistancemoment,compression,

    -bey

    *

    2y =bcy -6 X7400*20-25

    2 3 3

    -299,700 lb.xtreme fibre stress,nd

    although tronger n ension by this heory,

    only t'he weaker limi t can be reached, so

    that^

    we have a total

    of

    229,700 x2=599,40@ l b . ins.

    Then as

    9,990

    lb.

    in centre.

    B y

    the method

    of

    Fig. 4

    y=9-5.96=3.04 in.

    Resistance moment, compression=

    hey2- 6 x 7400 x 3 04'= 136,775.68 lb. in.

    3

    ~~

    3

    Resistance moment, tension

    =

    btX2- 6 X 14500X 9G2= 1,030,126.4 lb. in,

    3

    Together

    =

    1,166,902 lb. in.

    Then

    4 4

    l

    240

    By the method of Fig. 5

    W = - X

    R =

    -

    1,166,902=19,448 lb.

    in centre.

    y=9-3-04=5-96 in .

    Resistance nzonzent

    a s

    a couple.

    Compressive

    stress

    =----

    cy--6X7400X5.96-

    -

    2

    2

    132,312 lb.

    btx 6X14500X3*04-

    Tensile strength =-- =

    -

    2

    2

    132,240 lb. Average=132,276 lb.

    2

    Moment=132,276

    X

    X 9

    =

    793,656 lb. in.

    3

    in centre.

    By

    the method of Fig. 6

    3- 68 in. y=9-3.6 8=5-32 n,

    Resistance moment, conlpression

    =

    _ _ - _ _ _ _ ~ -

    ey - 6 x 7400 x 5 32'- 418,875.52 lb. in,

    3 8

    Resistame moment tension=

    b t 2- x 14500x 3

    68 =

    392,729.

    in,

    ...........

    3 3

    (would be equal if closer measure of x and

    y

    were taken.

    Together=811,605 lb. in.

    Sunmmry-

    By ratio

    from

    unit beanz=20266.2

    lb .

    .. Fig.

    3

    ..... = 9990.0 lb.

    ..

    Fig. 4

    ... ...

    =19448 4 lb.

    .. Fig. 5 ... ... =13227 6 lb.

    .. Fig . ...

    ... =

    13526 lb.

    E'oJlon-ing Sir 1-3. Baker's suggestion that

    the

    experimentm

    n

    unit beam gives an ap-

    p:trent excess strength

    of 70

    per cent., and

    reducing, W = --

    ._ which

    does

    not

    :lgree

    with ither

    of

    t~he

    previous

    results,

    so

    that we

    are

    st,ill

    without a n y p rw f

    of

    the position

    of

    the neutral axis.

    Kow take for

    example

    a nmterial stronger in

    compression thanension, sa y

    a cast

    iron

    beam 3 ft . pan, 1 in. road,

    2

    in. deep,

    loaded inhe entre ntilracture occurs.

    Ultimatr esistance

    t o

    direct ension

    7

    t'ons

    per sq. in., .compression

    42

    tons p e r sq. in . ,

    and

    '

    transverse

    loa,d

    for unit

    beam

    1

    ton. R y experiments on t h e trnnsveme

    20266.2 x 100- 11~)21r

    loo+70

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    6/8

    ~ _ _ _ _

    -

    f

    1'HE 1NSTiTUTION

    OF S T R U C T U R A L ENGINEERS. 2 7 9

    strength of cast iron beams

    of

    different

    mixtures,

    l

    in.quarend 2

    ft. 3

    in.

    between the upport s, he averagebreaking

    weight inheentre was

    1,000

    Ibs.he

    equivalent loador standardbeam

    1

    in.

    squareand

    1

    ft.

    span would be

    1000

    x

    -=

    2,250 bs. Otheresperinlents give 2,443 bs.

    as tln: average oad equired, nd vidently

    the'cc)mlnon rule th at 1 ton in the c.ent,re will

    justbreakacast iron bar 1 in. quareand

    1

    ft.

    span is about right.

    By themethod of Fig.

    3

    s = y = & d . = l n.

    rLesistance moment ension,

    btx'- l X 7 X l

    +

    tons,

    \ 27

    12

    -

    ~

    - ~ -

    3 3

    Together=41*33 ton ins.

    Then

    4

    l

    36

    W=--

    XR=-X41-33=4*59 ons=10281.6

    lb. in centre.

    By

    the method

    of

    Fig. 5a

    x= c xd=-

    c + t

    42 +7

    42 X2=1*714 =2-1.714=

    a286 in.

    Resistance nlonlent

    as a

    couple

    Conlpressive stress =

    -

    cy-1 X 42 X *286=6.006

    2

    tons.

    btx 1X7X1.*714-

    Tensile stress- - -999 tons.

    2

    L w d r

    t ons

    FIG. 7

    and his being the

    weaker limit, will be reached first, the stress on

    the opposite edge being equal the tot al will be

    2+ X 2 =4+ tons=10453; lb. Then as

    l 3 x 1 2

    Z C , TV=- 4R=;----x10453$= 4

    116'1 5 lb. in centre.

    By the method of Fig. 4a,

    7

    t + c

    7 +42

    x=-

    x d =

    -~

    2 = -2857 inches,y=2-

    2857=1.7143 in.

    Resistance nlomer,t, compression=

    ~-ey - 1X 42 X 1*7143"= 41.14on inS.

    3

    3

    Resistance moment, tension=

    btx'-

    1

    X 7

    X

    2857%= .

    19

    ton

    __-

    3 3

    Average=6*00 6+5~ g99= 6.00 25 ons.

    2

    Moment=6 0025 X X

    2

    =8a0033 ton ins.

    x R, . .W= 81 33= 8892 tons= 1991.8

    86

    lb. in centre.

    Then following Fig. 6a

    x= -

    d 7 i - 4 4 2

    2 x

    = 4798 in.nd y=d-x=2-

    .5798=

    1

    4202 in. The moment of resistance

    cbx

    42 X 1X 5798'= r

    t on

    to tension will be ~- =

    ins., and the moment of resistance to tension=

    3 3 4

    8

    3

    ~

    tbY2-7x1x1*4202' c 4 . 7 ton ins., but

    X

    36

    = 4 . 7 ~ 2 , .W=----=1-044 tons=2338 lb. n

    9.4

    9

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    -

    2 8 0 THESTRUCTURAL

    NGINEER:

    he

    Journal

    centre.Here agaiu theesults re ot suffi-

    ciently exact to prove anything.

    Summary :-

    27

    36

    12

    36

    12

    36

    By ratio from unit eam

    1000X

    2 =3000 lb.

    or 2240 X 2 =2984 lb

    or 2445

    X

    2'=3260 lb.

    By Fig. 3= 161 lb.

    ,, Fig. 4

    =10881 6

    lb.

    ,, Fig. 5 = 1991.8 lb .

    ,, Fig. 6 = 2338 lb.

    By Sir B. Baker's rule

    I n reinforced concrete beams where the con-

    crete is capable of bearing

    a

    maximum work-

    ing load in. compression of 600 lbs. per sq.

    in.,

    a~nd the steelmaximum tension of 16,000 lbs.

    per sq. in., verycareful tes ts were madeat

    th e ,M.cGill Un iwrs ity, Toronto of the posi-

    tion of theneutral axisundervarious oads.

    For small loads, abou t one-seventh of th e ulti-

    mat e, t v'as found o be a t 52 percent. of

    the dep th of the beam; while as the load in-

    creased the position of the neu tra l axis altered

    until it was only at 41 per cent.

    of

    the depth

    from the compression urface,where it e-

    ma,ined unti l the full1 load of one-third the ult i-

    mate was reached.

    I n this case the neutral axis starting in the

    cen tre of tbe beam, moved towards he edge

    of the weaker material as the stress increased,

    but

    it

    must be noted that this is also the com-

    pression side of t he beam.

    If

    we could determine he xtreme fibre

    stresses in a beam, we could obtain the corre-

    spondingelongation andshort,ening produced

    by

    direct stress, and from these find the radiu s

    of .curvatureand he position of theneutral

    axis,onverselyrom the elongation and

    shortening a t a given s tress we can determine

    thecurvatureundera load and hence he

    position

    of

    neutral axis.

    In th e experimentsmade by the Commis-

    sioners appointed to enquire into the Applica-

    tion of Iron to Railway Structures, the elonga-

    tionandshortening were ecorded ora bar

    of cast iron 1 in. square and 10 f t . long, from

    which Fig. 7

    is compiled. I n tension he bar

    broke with

    7.43

    tons,and he extension at

    6.6 ons

    was

    0.1859 in. I n corqxession he

    bar was so much undulated (although confined

    within limits) hat he estwas toppedat

    16.56 tons when t,he shorteningwas

    0.41149

    in.

    For comparisonwith the ension

    it

    maybe

    stated hatat6.44 ons he shorteningwas

    0.14163 n. In he diagram the extension s

    shown in open circles and the .conlpression in

    blackcircles of tlhesame scale of tons.

    T h e

    elongation

    or

    shortening by the fornzu a

    \\;here

    e=elongationnnches, w=loaci per

    sq. inectionalreanbs., =lengthn

    inches,E=modulus of elasticitynbs.

    =

    17,000,000 for cast iron, W O U ~ ~e

    instead of 0.1839 as found by tne experinlent

    inension. And

    e=

    14453~22X10X12_0~1020

    17,000,000

    instead of

    0.14163

    as found by the experiment

    in uol~pressionatabout he ame .load, o r

    37159*65X10X12-0,2623

    e =

    17,000,000

    instead of 0.41149 as found by the experiment

    in compression when the loading was stopped.

    The alculated xtension or compression is

    shownupon the diagramFig.

    7

    bya dotted

    line, h u t strictly hiscalculation holds good

    only up to the limit of elast icity.

    The resul ts of the experiments will be seen

    morelearlyrom ig. a,whichs to a

    smallerscale,and erminates .,vith thestress

    ut; which tens ile failure takes place.

    The conclusion from a study of the diagranl

    is that after about 2 ons per sq. in. the ex-

    tension ncreases ingreater proportion than

    the compression, up to, the . ' h i t of tensile

    strength, ndhathe eutral axis must ,

    therefore, shift nearer to th e compression side .

    B u t

    if

    the neutra l axis

    shifts,

    the stresses on

    theext reme fibres o,p andbottom,arenot

    equal,butmustbegreater on the weaker

    (tension)ide.henwhat happens ?Does

    the beam break by tension only. If so, is the

    extra strength in compression useless ?

    In the case

    of

    a cast irongirder

    of

    usual

    section, we have the neut,ral axis at d the e.g.

    of section, nd the tress ntens ity on the

    material proportioned

    to

    thedis tance of the

    part from the neutral axis.

    Clarke'sTheory of CastIronBeams(Min.

  • 8/16/2019 The Neutral Axis in Beam

    8/8

    o THE INST~TUTIONSTRUCTURALNGINEERS. 8

    Proc. Inst.

    C.E.,

    CXLIX,

    p. 313)

    stateshat cast

    i r o n does not

    follow Hooke's

    Ldw, andigh

    intensity of strain

    does not neces-

    sitate ropor-

    tionately high in-

    tensity of stress.

    I t ,h e r e f o r e .

    follows. with

    definite limiting

    stram OK stress n hoouter ensile fibres of

    the sect ion, the inner fibres which are strained

    proportionately to heir respectivedistances

    frum the neutra l axis are stressed to a higher

    degree than his and herefore have a higher

    moment,

    of

    resistancehanhat assigned

    them by the ordinary eamheory. More-

    over, if the tress tra in curves or ension

    and forompressionreotimilar, the

    ucutral axis will no longer remain central, but

    in a cast iron beam will sh if t slightdy towards

    the compressionside.This ncreases hearea

    under ensionandhence hesum of all the

    tensilestresses,and husraises hestrength

    of the beam t o resist fractu re. He then shows

    th at in a plain cast iron beam the neutral axis

    at fractu re is displaced by per cent. of the

    tolal depth of beam tcwhrds the co,mpression

    side, esultin? nan ncrease n treng th of

    41.1

    per cent.

    The esearches of Prof . Coker have shown

    conclusively tha t although the neu tra l axis is

    at the cen tr e of gravity of the section at the

    commencement of loading it is found to shift

    towards thestronger side as he loading n-

    crease s. Was it also in this case the compres-

    sion side ?

    Theres ne therupposition. uppose

    thecast iron beam o be nfinitelystrong n

    ccrnpression but comparativelyweak n en-

    sion, thenhe eut ral axis might e con-

    sidered to lie in the compressionedge of the

    FIG. 74

    beam and the failure to take plsce wholly by

    tension, as n Fig. 8. Thecalculation for our

    2 x 1 beam woulcl be

    ~

    X

    X 2

    =

    9% on ins. =20907 lb. ins. or

    W

    =

    20907 x

    =

    2323 lbs.,

    2 3

    36

    whichvirtuallyagreeswith the experiments

    oncross-breaking.

    Conclusions

    (a) The neutral axis shifts towards

    the

    coni-

    pressionside in cast ron, (b) it seems to be

    an established law that the stress in any fibre

    I

    h

    c

    FIG.8

    varies directly

    3s

    its distance from the neutral

    axis, (c) the stress on tension side ca,nnot ex-

    ceed 7 tons q. n., (d) a ouple must be

    formedwith equal. forces.

    Now in cast iron under the proved facts of

    (a) and (c), i t is clear tha t fo r (d) to take place

    (b) cannot occur.

    Where then is the neutral axis.?